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Thermal Environment of Launch Pads During Rocket Launching
Journal of Spacecraft and Rockets, 2022This paper investigates the thermal environment of launch pads during rocket takeoff. The rocket plume model is set up using the three-dimensional Navier–Stokes equations and realizable k−e turbule...
Chenyu Lu +3 more
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Rocket launch acoustics modeling
The Journal of the Acoustical Society of America, 2000The exhaust of a launch vehicle is composed of a high speed jet of gases that interact with the ambient air, the launch pad and the launch structure. This interacting flow is highly turbulent and is a significant source of sound power. Noise from the rocket plume can represent a threat to sensitive components on the vehicle and to the rocket payload (e.
Michael J. White, Gary M. Ogg
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Cornell Hotel and Restaurant Administration Quarterly, 1997
Revenue management (RM) is the application of disciplined tactics that predict consumer behavior at the micromarket level and optimize product availability and price to maximize revenue growth. While the application of RM principles depends on each company's competitive situation, the process is similar for all firms.
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Revenue management (RM) is the application of disciplined tactics that predict consumer behavior at the micromarket level and optimize product availability and price to maximize revenue growth. While the application of RM principles depends on each company's competitive situation, the process is similar for all firms.
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SAE Technical Paper Series, 1961
<div class="htmlview paragraph">This paper concerns a current Aerojet-General Corporation program to demonstrate the feasibility of servicing and launching liquid-propellant rockets floating in the sea, without the use of a special launching platform.
R.C. Truax, J.D. Ryan
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<div class="htmlview paragraph">This paper concerns a current Aerojet-General Corporation program to demonstrate the feasibility of servicing and launching liquid-propellant rockets floating in the sea, without the use of a special launching platform.
R.C. Truax, J.D. Ryan
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Solar System Research, 2019
In this paper, we examine a method for launching payloads from Mars, which is an alternative to a rocket launch. The idea is based on the elevator concept using a tether, one end of which is rigidly connected to the natural Martian satellite and the other end has a hook.
A. V. Bagrov, V. A. Leonov
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In this paper, we examine a method for launching payloads from Mars, which is an alternative to a rocket launch. The idea is based on the elevator concept using a tether, one end of which is rigidly connected to the natural Martian satellite and the other end has a hook.
A. V. Bagrov, V. A. Leonov
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Bungee jumping and rocket launching
International Journal of Educational Management, 2019Purpose A plethora of principal development programs based on myriad leadership theories currently abounds in many educational jurisdictions globally. Today’s principals, consequently and fortuitously, often feel less isolated and better supported that has been indicated in school leadership research over the past two decades.
Michael Christie +4 more
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Launch vehicle rocket propulsion improvement
37th Joint Propulsion Conference and Exhibit, 2001Reducing the cost of placing payloads in orbit depends greatly on reducing the weight & improving the performance of the launch vehicles including the Space Shuttle launch vehicle so that greater payloads may be carried. Improvement of the launch vehicle rocket motors is key to achieving the goal of greater payloads in orbit @ reduced cost.
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Trajectory Design of a Rocket–Scramjet–Rocket Multistage Launch System
Journal of Spacecraft and Rockets, 2017The integration of a reusable scramjet vehicle as the second stage of a multistage space launch system has the potential to reduce the cost of small-payload orbital launches.
Forbes-Spyratos, Sholto O. +3 more
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Numerical Simulation of Rocket Launch Vehicle
SSRN Electronic Journal, 2019Launching of Rocket is a complex phenomenon. There is high chance of failure in such missions. Hence it is necessary to predict the launch path or Trajectory, External disturbances and various other parameters. Numerical Simulation is one such way of predicting launch parameters which helps in taking precautions preventing failure.
Dhanush G J, +4 more
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Solid rocket motor space launch vehicles
Acta Astronautica, 1993Abstract Space launch vehicles based on solid rocket motors are more cost effective than liquid rocket engine boosters. When stringent performance and dimension (length and diameter) constraints can be relaxed, design and manufacturing margins can be increased.
A.J. MacLaren, H.D. Trudeau
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